Fuzzy-Based Adaptive Tracking Control for the Conversion Mode of Tilt-Rotor Aircraft

被引：0
|
作者：
Hu, Kaixuan [1 ]
Li, Wen [1 ]
Shi, Shuang [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Peoples R China
来源：
39TH YOUTH ACADEMIC ANNUAL CONFERENCE OF CHINESE ASSOCIATION OF AUTOMATION, YAC 2024 | 2024年
关键词：
Tilt-rotor aircraft; conversion mode; fuzzy logic systems; FLIGHT CONTROL; APPROXIMATION; DESIGN;
D O I：
10.1109/YAC63405.2024.10598456
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, a fuzzy-based adaptive tracking control scheme is proposed for the conversion mode of tilt-rotor aircraft subject to system uncertainties. In order to characterize the dynamics of the conversion process, a switched nonlinear model with respect to the inclination angle is established. To this end, an fuzzy control scheme is designed to enable the state of the closed-loop system to track the desired trajectory. Finally, the effectiveness of the proposed control method is illustrated by a simulation.
引用
收藏
页码：780 / 785
页数：6
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